20030904026729I

Incident · Minor damage

FAA incident report · Beech C23 · Newton, KS · September 4, 2003

Date
September 4, 2003 · 18:53 local
Place
Newton, KS
Airport
Newton-City-County Airport
Phase of flight
To Aborted (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N6723C
Reported as
Beech C23
Reported engine
Lycoming O360*
People aboard
1
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
29 total29 in this make and model26 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Pilot reported that during the landing phase, N6723C experienced excessive nose wheel shimmy. He then initiated take-off procedures by applying full power and partially retracting flaps. The pilot further reported that, even though he was applying back pressure on the yoke, the aircraft pitched down and he heard a "cracking sound". Pilot stated that he then removed power and applied forward yoke pressure. The inspection of the nose gear revealed that both lugs had been instantaneously overloaded. This information, supported by the pilot's statement, leads investigators to conclude that the aircraft's nose gear failed when the pilot reduced power and applied excessive forward pressure on the yoke. privacy data omitted

As the FAA filed it

(-23) PILOT REPORTED THAT DURING THE LANDING PHASE, N6723C EXPERIENCED EXCESSIVE NOSE WHEEL SHIMMY. HE THEN INITIATED TAKE-OFF PROCEDURES BY APPLYING FULL POWER AND PARTIALLY RETRACTING FLAPS. THE PILOT FURTHER REPORTED THAT, EVEN THOUGH HE WAS APPLYING BACK PRESSURE ON THE YOKE, THE AIRCRAFT PITCHED DOWN AND HE HEARD A "CRACKING SOUND". PILOT STATED THAT HE THEN REMOVED POWER AND APPLIED FORWARD YOKE PRESSURE. THE INSPECTION OF THE NOSE GEAR REVEALED THAT BOTH LUGS HAD BEEN INSTANTANEOUSLY OVERLOADED. THIS INFORMATION, SUPPORTED BY THE PILOT'S STATEMENT, LEADS INVESTIGATORS TO CONCLUDE THAT THE AIRCRAFT'S NOSE GEAR FAILED WHEN THE PILOT REDUCED POWER AND APPLIED EXCESSIVE FORWARD PRESSURE ON THE YOKE. ^PRIVACY DATA OMITTED^

Other reports on N6723C · 2

Matched to the same aircraft by N-number and date.